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Die Identifizierung einer Koeffizientenfunktion (Identification of a Coefficient Function)
Influence of Elasticity on the Lifting Force of a Wing
A Method of Approximation for Calculating the Orbits of Space Rockets
Numerical Solutions of Inherently Unstable Ordinary Differential Equations
Transient Response of Butterworth Approximations of Ideal Low-Pass Filters
On the Question of the Solution of a Differential Equation of the Form X + p(T)X = 0
Two-Dimensional Jet Control. Part 1 - a Plane Jet in a Stationary Oblique Flow - Theory
Certain Problems of Rendezvous of a Space Vehicle with an Orbital Station
Stability and Control Derivatives of the De Havilland DHC-2 'BEAVER' Aircraft
About a Method of Numerical Solution of Nonlinear Systems
Question of Gas Motion near Strongly Heated Bodies
Transport of Solids by Pipeline Annual Report, 1 Apr. 1967 - 31 Mar. 1968
Point-Mass Aircraft Trajectory Prediction Using a Hierarchical, Highly-Adaptable Software Design
Nutational Stability of a Dual-Spin Satellite under the Influence of Applied Reaction Torques
Some Considerations on the Problem of Non-Steady State Traffic Flow Optimization
A Direct Direction-Doppler Slant-Range Determination Technique for Orbiting Space Vehicles
The Numerical Solution of Partial Differential Equations Governing Convection
Integrated Navigation, Guidance, and Control of Missile Systems: 2-D Dynamic Models
Accuracy of Interpolated and Differentiated Satellite Positions
Study of Some Stream Functions for the Determination of Transonic Flows past Airfoils
The Perturbation of Pendulum and Gyroscope Instruments by Acceleration of the Vehicle
Zur Berechnung von Nichtlinearen Schwingungen (Calculation of Non Linear Oscillations)
The Solution of a Satellite Re-Entry Problem by a Gradient Technique
Application of a Mechanical Gyroscopic Stabilizer to VTOL Aircraft
Study of APOLLO Water Impact. Volume 7 - Modification of Shell of Revolution Analysis Final Report
On Some Possible Simplifications and Changes in Hansen'S Lunar Theory
Supersonic Flow-Around of Thin Bodies with Mach Number Close to Unity
Aeroelasticity of Axially Loaded Aerodynamic Structures for Truss-Braced Wing Aircraft